(7)
On the panel 24VU, release the FLT CTL/FAC2 pushbutton switch (on this pushbutton switch, the OFF legend comes on).
(8)
Install the PIN - RIGGING (98D27207547000) (48) or RIGGING PIN SET (98D27207516000) pin (98D27207516160) on the cable quadrant (45). (Refer to Detail Q).
(9)
Put the PIN, RIGGING - RUDDER CONTROL (98A27901002000) (2) on the input lever of the tension regulator (1). (Refer to Details G and A).
(10)
Depressurize the Blue hydraulic system (Ref. TASK 29-10-00-864-003).
(11)
De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
(12)
Put warning notices on the CAPT and F/O rudder pedals.
1EFF : ALL 1 27-21-61Page 416 1 1 May 01/05R 1 1 1CES 1
4. Procedure
_________
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 401/TASK 27-21-61-991-001) R **ON A/C 151-199, 401-499,
(Ref. Fig. 401A/TASK 27-21-61-991-001-A)
**ON A/C 301-399,
(Ref. Fig. 401B/TASK 27-21-61-991-001-B)
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 402/TASK 27-21-61-991-002) R **ON A/C 151-199, 401-499,
(Ref. Fig. 402A/TASK 27-21-61-991-002-A)
**ON A/C 301-399,
(Ref. Fig. 402B/TASK 27-21-61-991-002-B)
**ON A/C ALL
(Ref. Fig. 403/TASK 27-21-61-991-003, 404/TASK 27-21-61-991-006, 405/TASK 27-21-61-991-004, 406/TASK 27-21-61-991-005)
Frame Feed-Through Fittings Figure 405/TASK 27-21-61-991-004
1EFF : 1 1R 1CES ALL 1 11 1 27-21-61 Page 418 May 01/05
Pulley Figure 406/TASK 27-21-61-991-005
R 1EFF : 1 1 1CES ALL 1 111 27-21-61 Page 419 May 01/05
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-21-61-020-053
A. Removal of the Rudder Control Cables (Forward Part)
(1)
Removal of the turnbuckles.
(a)
Remove the locking clips (33) from the turnbuckles (34) (Refer to Detail L).
(b)
Turn the turnbuckles (34) until you can install the TOOL -LOCKING (FE171901) (18) on the tension regulator (1).
(c)
Install the TOOL - LOCKING (FE171901) (18) on the tension regulator (1) with the pins (17).
(d)
Remove and discard the cotter-pins (6) from the cable-end holders of the tension regulator (1) (Refer to Details C and D).
(e)
Remove the turnbuckles (34).
(2)
Removal of the cable guides on frames 35, 33, 28, 23 and 14 (refer to detail K).
(a)
Cut and discard the cable ties (32).
(b)
Remove the locking devices (31).
(c)
Remove the half shells (30).
(3)
Removal of the cables from the tension regulator.
(a)
Remove and discard the cotter-pin (11), remove the nut (10) and the washer (9) (Refer to Detail E).
(b)
Remove the bolt (7) and the spacer (8) from the pulley casing (3).
(c)
Remove and discard the cotter-pins (16), remove the nuts (15) and the washers (14) (Refer to Detail F).
(d)
Remove the bolts (12) and the spacers (13). CAUTION : MONITOR THE END OF THE CABLE WHEN YOU PULL IT.
_______
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-21-61Page 420 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
(e) Remove the cables (4) and (5) from the tension regulator (1) and pull them. (Refer to Details C and D).
**ON A/C 301-399,
Subtask 27-21-61-020-053-A
A. Removal of the Rudder Control Cables (Forward Part)
(1)
Removal of the turnbuckles.
(a)
Remove the locking clips (33) from the turnbuckles (34) (Refer to Detail L).
(b)
Turn the turnbuckles (34) until you can install the TOOL -LOCKING (FE171901) (18) on the tension regulator (1).
(c)
Install the TOOL - LOCKING (FE171901) (18) on the tension regulator (1) with the pins (17).
(d)
Remove and discard the cotter-pins (6) from the cable-end holders of the tension regulator (1) (Refer to Details C and D).
(e)
Remove the turnbuckles (34).
(2)
Removal of the cable guides on frames 35.3, 33, 28, 23 and 14 (refer to detail K).
(a)
Cut and discard the cable ties (32).
(b)
Remove the locking devices (31).
(c)
Remove the half shells (30).
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵2(62)
